View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 14506U 83113A 25193.69621869 .00000145 00000-0 72922-4 0 9995
2 14506 98.3786 345.9884 0011500 148.3201 222.2592 14.29565519166987
Epoch (UTC): | 12 July 2025 16:42:33 |
Eccentricity: | 0.0011500 |
inclination: | 98.3786° |
perigee height: | 785 km |
apogee height: | 801 km |
right ascension of ascending node: | 345.9884° |
argument of perigee: | 148.3201° |
revolutions per day: | 14.29565519 |
mean anomaly at epoch: | 222.2592° |
orbit number at epoch: | 16698 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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